View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 58727U 26145.63590800 +.00000000 +00000-0 +37108-3 0 00003
2 58727 97.5398 219.4715 0013517 38.0812 322.1376 15.20829777 02
| Epoch (UTC): | 25 May 2026 15:15:42 |
| Eccentricity: | 0.0013517 |
| inclination: | 97.5398° |
| perigee height: | 494 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 219.4715° |
| argument of perigee: | 38.0812° |
| revolutions per day: | 15.20829777 |
| mean anomaly at epoch: | 322.1376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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